RU2562774C2 - Shooting-control informating-controlling system - Google Patents

Abstract

FIELD: weapons and ammunition.

SUBSTANCE: system comprises computer-aided operator workstation, two computer complexes, two keyboards, two documentation devices, two monitors, two basic stations of common-timing system with companion antennas, data exchange digital channels, peripheral subsystems of communication, control devices, main and slave control units, drive motors of current interrupters, operation checkup units, power supply devices, main and slave switching units, main and slave units of secondary power supplies, main and slave units to output commands for operation of pyrocartridges, main and slave units of discharging, main and slave units for supply of current interrupters drive motors, main and slave units of keep-alive electric supply.

EFFECT: enhanced performances, higher safety, reliability and fault-tolerance in missile control and launching.

1 dwg

Description

The invention relates to combat information and control systems and can be used to control the preparation and launch of missiles (anti-missiles, torpedoes, guided missiles, etc.) into which the flight mission data is input from supporting systems.

A device is known - an automated air defense fire control system that contains an electronic computer, data transmission equipment, technical means of automating the maintenance of fire weapons, a multichannel switching device for their electrical interfacing with targeting radar and fire tools (IPC G06F 19/00, G06F 171: 00, G06F 13/00, RF patent No. 22218598, publ. 07.20.2003).

The disadvantages of this device are the limited functionality for the preparation and launch of missiles (missiles, torpedoes, guided missiles, etc.), requiring accurate time synchronization with the operation of the targeting radar and fire weapons, insufficient reliability and fault tolerance in the event of exit building individual elements of the system.

A device is also known - command-firing information management system (IPC G06F 15/16, RF patent No. 58748, publ. November 27, 2006).

The device comprises an operator panel consisting of two electronic computers, two system interface lines, four adapters for a multiplex communication channel, a keyboard, a graphic information display device, two digital input-output devices, a control and control panel, a lag interface adapter and a serial adapter interface, information exchange highway in the form of a redundant multiplexed information exchange channel, at least one peripheral device communication with control objects, each of which contains an electronic computer of a peripheral communication device with control objects, a system interface highway of a peripheral communication device with control objects, an adapter of the multiplex channel of information exchange of a peripheral communication device with control objects, an adapter of code communication channels with control objects, a digital input-output device for a peripheral communication device with control objects and m relay blocks.

The device has:

- limited functionality for the preparation and launch of missiles (missiles, torpedoes, guided missiles, etc.), requiring precise time synchronization with the operation of external systems and control objects;

- a low degree of security from unauthorized control actions (from supporting systems, the operator, environmental factors, enemy forces and equipment, emergency situations caused by equipment failures, etc.) and / or during missile launch failures (missile defense, torpedoes , guided missiles, etc.), for example, due to a malfunction of relay blocks;

- insufficient reliability of operation and fault tolerance of the operator console in case of failure of its individual elements.

The closest prototype to the claimed technical solution is a device - firing command and control information system (IPC G06F 19/00, G06F 171: 00, G06F 15/16, RF patent No. 2191430, publ. 20.10.2002).

This device contains an operator console consisting of two electronic computers, two system interface lines, four LAN adapters, a keyboard, a documentation device, a monitor, a video adapter, a multiplex channel adapter, a long-term storage device, a digital I / O adapter, and a control panel

and control, a parallel interface adapter and a serial interface adapter, two interface lines of information exchange, two peripheral devices for communication with control objects, each of which contains a calculator module, start circuit modules, and onboard equipment power modules.

This device solves the problem of controlling the preparation and launch of missiles (anti-missiles, torpedoes, guided missiles, etc.) when automatically entering flight mission data from supporting systems, but its disadvantages are:

- limited functionality that does not allow it to be used for the preparation and launch of missiles (anti-missiles, torpedoes, guided missiles, etc.) requiring precise time synchronization of the preparation and launch operations, including data input of the flight mission, with the work of the supporting systems, as well as the exact implementation of a certain time schedule (time reference: maternity, astronomical, relative, etc.) prelaunch preparation and launch;

- a low degree of security that does not allow it to be used for the preparation and launch of missiles (anti-missiles, torpedoes, guided missiles, etc.) requiring protection from unauthorized control actions (from supporting systems, the operator, environmental factors, forces and means of the enemy , emergency situations caused by equipment failures, etc.) by physically breaking the start circuit modules and on-board equipment power modules from the firing command and control information system from the r kw (missiles, torpedoes, guided missiles and the like), and perform special demolition operations, including the discharge of onboard power sources for missiles (anti-missile, guided missile torpedoes, etc.), in the event of a failed launch;

- insufficient reliability of operation and fault tolerance, not allowing it to be used for the preparation and launch of missiles (anti-missiles, torpedoes, guided missiles, etc.) requiring systematic implementation

autonomous, according to the operator’s commands, and complex, according to the commands from the supporting systems, functional tests (testing) of the firing command and control information system, including with imitation of missile preparation and launch operations (missile defense, guided missile torpedoes, etc.).

The technical task of the claimed invention is the creation of a device - command-firing information-control system, which allows you to expand the functionality, improve the safety, reliability and fault tolerance of combat information-control systems designed to control the preparation and launch of missiles (missiles, torpedoes, guided missiles, etc.) .P.).

The problem is solved as follows.

In the device - firing command and control information system, containing the operator’s workstation (operator’s console), equipped with two computer systems (electronic computers), two keyboards, two documentation devices and two monitors, peripheral communication subsystems according to the number of missiles being prepared for launch (missiles, torpedoes, guided missiles, etc.), digital channels of information exchange in an amount corresponding to the number of peripheral subsystems communications or a multiple of the number of peripheral communication subsystems are additionally introduced into the operator's automated workstation - two base stations of the same time system with external antennas, each control peripheral subsystem - a control device consisting of a main and backup control units, a motor drive of current disconnectors and a functional check unit , power supply device, consisting of the main and backup blocks of switching, the main and backup blocks of secondary sources power supply, the main and backup power supply units for triggering the squibs, the main and backup power units of the discharge, the main and backup power supplies of the motor drive of current disconnectors, the main and backup power supply units on the standby, and to each computer complex from the operator’s automated workstation using digital channels information exchange connected keyboard, documentation device, monitor, base station of the system of a single time with remote by antennas, through the first groups of inputs, the main / duplicate control units and the function test blocks from the control devices of the peripheral communication subsystems, each power supply device from the peripheral communication subsystems through the inputs of the main and backup blocks of secondary power supplies, the main and backup blocks of command issuance for igniter activation , the main and backup power supply units of the motor drive of current disconnectors, the main and backup power supply standby units connected to an external power source, the outputs of the main and backup power supply standby units are connected to consumers from the power supply and control devices, the outputs of the main and backup power supply units of the motor drive of current disconnectors, the main and backup power supply units for actuating the igniter, the main and backup power supply units connected respectively to the fourth inputs, the sixth and seventh groups of inputs of the main and backup switching blocks ii, the fifth groups of outputs connected to the inputs of the main and backup blocks of the discharge, the second groups of outputs to the tenth and twelfth groups of inputs of the motor drive current disconnectors, the third groups of inputs of the main and backup blocks of switching connected to the fourth groups of outputs of the main and backup control units, and the first groups of inputs - to the ninth and eleventh groups of outputs of the motor drive of current disconnectors, each of the main and duplicate control units of control devices from the peripheral communication subsystems by the second groups of outputs and the third groups of inputs are connected to the mating elements of the firing command and control information system (for example, doors, hatches, security devices, microclimate support devices, etc.), by the fifth groups of outputs to the first and eighth groups inputs of the motor drive of current disconnectors, sixth groups of inputs to the second and seventh groups of outputs of the motor drive of current disconnectors, each of the motor drives of current disconnectors of control devices from the composition of the peripheral communication subsystems, the sixth group of inputs and the fifth group of outputs are connected to a rocket (anti-missile, torpedo, guided missile, launch container, etc.), and the third group of inputs and the fourth group of outputs are connected respectively to the second group of outputs and the third group inputs of the functional check unit.

The set of distinctive features of the claimed invention ensures the implementation of the technical task.

From the studied scientific, technical and patent information, the authors do not know the device with the distinguishing features indicated in the claims, this gives reason to conclude that the claimed object meets the criteria of the invention.

In FIG. 1 presents a functional diagram of the claimed invention.

Device - firing command and control information system contains an automated workstation of the operator (operator console) 1, equipped with the first 2 and second 3 computing complexes (electronic computers), the first 4 and second 5 keyboards, the first 6 and second 7 documentation devices, the first 8 and second 9 monitors, the first 10 and second 11 base stations of the single time system with remote antennas, from two to 2n digital channels of information exchange 12 _1-1 ÷ 12 _1-n , 12 _2-1 ÷ 12 _1-n , from one up to n identical to the periphery communication subsystems 13 ₁ ÷ 13 _n , each of which has a control device 14, consisting of a main 15 and a backup 16 control units, a motor drive of current disconnectors 17 and a functional check unit 18, a power supply device 19, consisting of a main 20 and a backup 21 switching units primary 22 and duplicating 23 secondary blocks

power supplies, the main 24 and the backup 25 blocks of command for triggering the igniter, the main 26 and the backup 27 blocks of the discharge, the main 28 and the backup 29 power supply units of the motor drive current disconnectors, the main 30 and the backup 31 units of standby power supply.

At the same time, the first keyboard 4, the first documenting device 6, the first monitor 8, the first base station of the single time system 10 with a remote antenna are connected to the first computing complex 2 from the automated workstation of operator 1 using digital information channels using digital information channels exchange 12 _1-1 ÷ January _12-n through the first group of inputs-outputs 15 and core redundant control units 16 and the operation check blocks 18 from the peripheral control devices 14 odsistem connection 13 ₁ ÷ 13 _n, to the second computer complex 3 from the workstation operator 1 by digital traffic channels connected to the second keyboard 5, a second device document 7, a second monitor 9, the second single-time system, the base station 11 to remote antenna , using the digital channels of information exchange 12 _2-1 ÷ 12 _2-n through the first groups of inputs and outputs, the main 15 and duplicating 16 control units, as well as functional check units 18 of the control devices 14 peripheral communication subsystems 13 ₁ ÷ 13 _n , each power supply device 19 from the composition of peripheral communication subsystems 13 ₁ ÷ 13 _n through the inputs of the main 22 and the backup 23 blocks of secondary power supplies, the main 24 and the backup 25 power supply units for the operation of the igniter, the main 28 and duplicating 29 power supply units of the motor drive of current disconnectors, the main 30 and backup 31 power supply units on the standby is connected to an external power supply 34 _i , the outputs of the main 30 and backup power supply units 31 on 31 The power supply is connected to consumers from the power supply device 19 and control unit 14, the outputs of the main 28 and the backup 29 power supply units of the motor drive of current disconnectors, the main 24 and the backup 25 power supply units for actuating the igniter, the main 22 and the backup 23 power supply units 23 are connected respectively to the fourth inputs, the sixth and seventh groups of inputs of the main 20 and the backup 21 switching units, the fifth groups of outputs are connected to the inputs of the main 26 and duplicating 27 blocks series, the second groups of outputs - to the tenth and twelfth groups of inputs of the motor drive of current disconnectors 17, the third groups of inputs of the main 20 and the backup 21 switching units are connected to the fourth groups of outputs of the main 15 and the backup 16 control units, and the first groups of inputs - to the ninth and eleventh groups outputs of the motor drive of current disconnectors 17, each of the main 15 and duplicating 16 control units of control devices 14 from the composition of the peripheral communication subsystems 13 ₁ ÷ 13 _{n by the} second groups of outputs and third upy inputs connected to the mating elements of the command-firing information-control system (for example, doors, hatches, protective devices, devices for maintaining the microclimate, etc.) 33 _i , the fifth groups of outputs to the first and eighth groups of inputs of the motor drive current disconnectors 17, six groups of inputs - for the second and seventh groups tokorazediniteley outputs motor drive 17, each motor 17 drives tokorazediniteley control device 14 from the peripheral communication subsystem 13 ÷ ₁₃ January sixth _n Rupp inputs and outputs of the fifth group is connected to the rocket (interceptor missiles, torpedoes, guided missiles, launch canister, etc.) 32 _i, and inputs the third group and fourth group of outlets connected respectively to the outputs of the second group and third group of inputs of the verification unit 18 .

The operating procedure of the device is divided into stages:

- preparatory;

- on duty;

- main;

- emergency;

- Maintenance.

Preparatory stage

The first 2 and second 3 computing complexes (electronic computers), the first 6 and second 7 documentation devices, the first 8 and second 9 monitors, the first 10 and second 11 base stations of the single time system with remote antennas from the automated workstation of the operator (operator console ) 1 are connected to external power sources.

Power supply devices 19 from the composition of peripheral communication subsystems 13 ₁ ÷ 13 _n through the inputs of the main 22 and duplicating 23 blocks of secondary power supplies, the main 24 and duplicating 25 blocks of command for triggering the igniter, the main 28 and duplicating 29 power supplies of motor drives of current disconnectors, the main 30 and duplicate 31 standby power supply units are connected to external power supplies 34 ₁ ÷ 34 _n .

Electricity consumers from the composition of control devices 14 and power supply 19 are connected to the outputs of the main 30 and backup 31 power supply units from the composition of power devices 19 of the peripheral communication subsystems 13 ₁ ÷ 13 _n .

When power is supplied to the first 2 and second 3 computing complexes (electronic computers), the first 6 and second 7 documentation devices, the first 8 and second 9 monitors, the first 10 and second 11 base stations of the single time system with remote antennas from the workstation operator 1 and to the inputs 30 and core redundant standby power supply 31 from the power supply device 19, the peripheral communication subsystem 13 ₁ ÷ 13 _n is initialized to a preset first 2 and second 3 computable itelnyh complexes from the automated operator position 1, the top 15, duplicate control units 16 and the operation check blocks 18 from the control device 14, the peripheral communication subsystem 13 ₁ 13 ÷ _n, functional software purpose firing command and information management system. In this case, it is carried out:

a) the conversion of primary electricity (AC voltage) supplied to the inputs of the main 22 and duplicating 23 blocks of secondary power supplies, the main 24 and duplicating 25 blocks of command for triggering the squibs, the main 28 and duplicating 29 power supplies of motor drives of current isolators into DC voltages with characteristics required for launching missiles (missiles, torpedoes, guided missiles and the like) 32 ₁ 32 ÷ _n and safe operation of the command-purpose firing control information yoke which are supplied respectively to the seventh, sixth and fourth main group 20 of inputs and the backup blocks 21, switching from the power supply device 19, the peripheral communication subsystem ₁₃ January 13 ÷ _n;

b) the conversion of primary electricity (AC voltage) supplied to the inputs of the main 30 and the backup 31 power supply units from the power supply devices 19 to a DC voltage with the characteristics necessary for the safe operation of the firing command and control information system, which is supplied to consumers of electricity from the control device 14 and power supply 19 of peripheral communication subsystem ₁₃ January 13 ÷ _n;

c) automatic testing and preparation for the operation of hardware and software:

- the first 2 and second 3 computing complexes, the first 4 and second 5 keyboards, the first 6 and second 7 documentation devices, the first 8 and second 9 monitors, the first 10 and second 11 base stations of the single time system with remote antennas from the automated workstation of the operator one;

- the main 15, duplicating 16 control units and a functional check unit 18 of the control devices 14 of the peripheral communication subsystems 13 ₁ ÷ 13 _n ;

d) in the dialogue mode “operator - computer complex” using the first 4 and second 5 keyboards, the operator manually enters access passwords (the implementation of the functions of software restricting operator access to the functional software of the firing command and control information system);

e) under the control of the functional software of the firing command and control information system or the system software of the first 2 and second 3 computing complexes, automatic testing of digital channels of information exchange 12 _1-1 ÷ 12 _1-n , 12 _2-1 ÷ 12 _2-n organization of information exchange:

- through digital channels of information exchange 12 _1-1 ÷ 12 _1-n between the first computer complex 2 of the automated workstation of operator 1 and the main 15, duplicating 16 control units and functional check units 18 of the control devices 14 of peripheral communication subsystems 13 ₁ ÷ 13 _n ;

- through digital channels of information exchange 12 _2-1 ÷ 12 _{2-n to the} honey of the second computing complex 3 from the automated workstation of the operator 1 and the main 15, duplicating 16 control units and functional check units 18 of the control devices 14 of the peripheral communication subsystems 13 ₁ ÷ 13 _n ;

f) under the control of the functional software of the firing command and control information system or the system software of the first 2 and second 3 computing complexes, automatic synchronization of the time generated by the first 2 and second 3 computing complexes with the time generated, respectively, of the first 10 and second 11 base stations of a single time system with remote antennas from the automated workstation of operator 1;

g) in the dialogue mode “operator - computer complex” using the first 4 and second 5 keyboards, the operator manually entered into the memory of the first 2 and second 3 computer complexes from the automated workstation of operator 1 data on the firing command and control information system, peripheral subsystems communications 13 ₁ ÷ 13 _n , missiles (anti-missiles, torpedoes, guided missiles, launch containers, etc.) 32 _l ÷ 32 _n and the operator of the firing command and control information system;

h) under the control of the functional software of the firing command and control information system, automatic or by the operator, in the dialogue mode “operator-computer complex” using the first 4 and second 5 keyboards from the automated workstation of operator 1, manual assignment of the first computer complex 2 - main, and the second computing complex 3 - duplicate, or, conversely, the main computing complex with installed on it part of the functional software This support provides further control over the operation of the firing command and control information system as a whole, while the backup provides control over the current technical condition of the digital channels of information exchange associated with it (12 _1-1 ÷ 12 _1-n or 12 _2-1 ÷ 12 _{2 -n} ) and peripheral communication subsystems 13 ₁ +13 _n ;

i) sequentially, for each peripheral communication subsystem 13 ₁ ÷ 13 _n , automatically under the control of the functional software of the firing command and control information system, or manually by the operator, in the dialogue mode “operator - computer complex” using the first 4 and second 5 keyboards from the automated workstation of operator 1 (signal transceiver between the first 2 or second 3 computing complex and the main 15, duplicating 16 control units and function check units tion 18 from the control device 14 through the digital traffic channels 12 _1-1 ÷ January _12-n or _2-1 ÷ 12 Feb. _12-n) is carried out:

- determination of the initial position of the motor drive of the current disconnectors 17 from the control device 14 issuing from the fifth groups of outputs of the main 15 and / or the backup 16 control units from the control device 14 of the discrete signals, respectively, to the first and / or eighth groups of inputs of the motor drive of the current disconnectors 17 s subsequent reading from sixth groups of inputs of the main 15 and / or backup 16 control units from the control device 14 discrete signals received, respectively, from the second th and / or seventh groups of outputs of the motor drive of current disconnectors 17 (Algorithm 1);

- if the motor drive of the current disconnectors 17 from the control device 14 is not in a position in which the fifth groups of outputs and sixth groups of inputs of the main 15 and the backup 16 control units from the control device 14, the second groups of outputs and the first groups of inputs of the main 20 and the backup 21 the switching units of the power supply device 19 are connected through a motor drive of the current disconnectors 17, respectively, to the third group of inputs and the second group of outputs of the functional check unit 18 from leaving the control device 14, the motor drive of the current disconnectors 17 is transferred to the required position: from the fourth groups of outputs of the main 15 and / or the backup 16 control units, discrete signals are output from the control device 14 to the third groups of inputs, respectively, of the main 20 and / or backup 21 switching units from the power supply device 19, in which the switching elements (relays, contactors, power switches, etc.) are triggered, which ensures the transfer of control discrete signals for changing the position of the motor drive of current disconnectors 17 from the main 28 and / or backup 29 power supply units of the motor drive of current disconnectors from the power supply device 19, supplied to the fourth inputs of the main 20 and / or duplicating 21 switching units, through the second groups of outputs of the main 20 and / or duplicating 21 switching blocks from the power supply device 19 to tenth and / or twelfth groups of inputs of the motor drive of current disconnectors 17 (Algorithm 2);

- checking the position of the motor drive of current disconnectors 17 from the control device 14, in which the fifth groups of outputs and sixth groups of inputs of the main 15 and the backup 16 control units from the control device 14, the second groups of outputs and the first groups of inputs of the main 20 and the backup 21 switching blocks from the composition of the power supply device 19, respectively, are not connected through the fifth group of outputs and the sixth group of inputs of the motor drive of current disconnectors 17 with a missile (anti-missile, torpedo, control by direct projectile launch canister, etc.) 32 _i, for which outputs from the fifth main group 15 and / or the backup control unit 16 from the control device 14 are issued digital signals respectively into first and / or the eighth group of the motor actuator inputs current isolators 17 with subsequent reading from sixth groups of inputs of the main 15 and / or backup 16 control units from the control device 14 of discrete signals received, respectively, from the second and / or seventh groups of outputs of the motor drive drive Unifiers 17 (Algorithm 3);

- checking the serviceability of the switching elements from the main 20, duplicating 21 switching units, as well as checking the serviceability of the main 22, duplicating 23 blocks of secondary power supplies, the main 24 and duplicating 25 command supply units for the operation of the squibs from the power supply device 19, for which from the fourth output groups of the main 15 and / or backup 16 control units from the control device 14 discrete signals are output to the third input groups, respectively, of the main 20 and / or backup 21 units switching commutations from the power supply device 19, in which switching elements are turned on and then turned off, and when switching on the switching elements, the appearance of discrete or analog signals is recorded on the third group of inputs of the functional check unit 18 from the control device 14, coming from the main 22 or backup 23 blocks of secondary power supplies, or from the main 24 or a backup of 25 blocks for commanding the activation of igniters from the power supply device 19 through the sixth and seventh groups of inputs, the second group of outputs of the main 20 and / or the backup 21 switching units from the power supply device 19, respectively, the tenth and twelfth group of inputs, the fourth group of outputs of the motor drive current disconnectors 17 from the control device 14; when switching off the switching elements, the loss of discrete or analog signals is recorded on the third group of inputs of the functional check unit 18 from the control device 14 (Algorithm 4);

- checking the serviceability (current state) of the mating elements of the firing command and control information system (for example, doors, hatches, security devices, microclimate maintaining devices, etc.) 33 _{i by} issuing from the second groups of outputs and reading from the third groups of inputs of the main 15 and / or duplicating 16 control units from the control device 14 discrete and analog signals (Algorithm 5);

- checking the sequence and correctness of the operations for preparing and launching a rocket (anti-missile, torpedo, guided missile, etc.) 32 _i , for which, in accordance with the training and launch sequence diagram, implemented as part of the functional software for command-fire information and control system: from the fourth groups of outputs of the main 15 and / or the backup 16 control units from the control device 14, discrete signals to / from the third (s) group are issued / removed in the required sequence the inputs, respectively, of the main 20 and / or duplicating 21 switching units from the power supply device 19, in which the switching elements are turned on / off, which ensures the appearance / disappearance of discrete and / or analog signals on the third group of inputs of the operation check unit 18 from the device control 14 coming from the main 22 and / or duplicating 23 blocks of secondary power supplies, and / or from the main 24 and / or duplicating 25 blocks of command for triggering the igniter through the sixth seventh input group, the second main group 20 and / or 21 of the backup switching units output from the power device 19, respectively, tenth and twelfth input group, the fourth group motor drive tokorazediniteley outputs 17 from the control device 14; from the fifth groups of outputs of the main 15 and / or the backup 16 control units from the control device 14, discrete and / or analog signals are received / removed in the required sequence, which are transmitted to the third group of inputs of the function check unit 18 from the control device 14 through the first and / or the eighth group of inputs, the fourth group of outputs of the motor drive current disconnectors 17 from the control device 14; the function check unit 18 of the control device 14, depending on the signals arriving at the third group of inputs, generates signals at the second group of outputs, which through the third group of inputs, the second and seventh group of outputs of the motor drive of the current disconnectors 17 go to the sixth group of inputs of the main 15 and / or duplicating 16 control units from the control device 14; discrete and analog signals are inputted to the sixth groups of inputs of the main 15 and / or the backup 16 control units from the control device 14 (Algorithm 6);

- checking the health of the motor drive of current disconnectors 17 from the control device 14, for which it is consistent: from the fourth groups of outputs of the main 15 and / or the backup 16 control units from the control device 14, discrete signals are output to the third groups of inputs, respectively, of the main 20 and / or duplicating 21 switching units from the composition of the power supply device 19, in which the switching elements are triggered, which ensures the transmission of control discrete signals to change the position d drive drive of current disconnectors 17 from the main 28 and / or backup 29 power supply units of the motor drive of current disconnectors from the power supply device 19 supplied to the fourth inputs of the main 20 and / or backup 21 switching units, through the second output groups of the main 20 and / or backup 21 switching units from the composition of the power supply device 19, respectively, to the tenth and / or twelfth groups of inputs of the motor drive current disconnectors 17; checking the execution of the command to change the position of the motor drive of the current disconnectors 17 from the control device 14, in which the fifth groups of outputs and sixth groups of inputs of the main 15 and the backup 16 control units from the control device 14, the second groups of outputs and the first groups of inputs of the main 20 and backup 21 switching units from the power supply device 19, respectively, are connected through the fifth group of outputs and the sixth group of inputs of the motor drive current disconnectors 17 with a missile (a missile defense, a torpedo guided by a projectile, a launch container, etc.) 32 _i , for which, from the fifth output group of the main 15 and / or the backup 16 control units from the control device 14, discrete signals are output, respectively, to the first and / or the eighth group of inputs of the motor drive of the current disconnectors 17, followed by reading from the sixth groups of inputs of the main 15 and / or the backup 16 control units from the control device 14 of the discrete signals received, respectively, from the second and / or seventh output groups of the motor drive current disconnectors 17; the type and correctness of the connection of the missile (anti-missile, torpedo, guided missile, launch container, etc.) is checked 32 _i , for which, from the fifth output group of the main 15 and / or the backup 16 control units, discrete signals are issued from the control device 14, respectively, to the first and / or eighth groups of inputs and then from the fifth group of outputs of the motor drive of the current disconnectors 17 to the missile (anti-missile, torpedoes, guided missile, launch container, etc.) 32 _i , followed by reading from sixth g a group of inputs of the main 15 and / or the backup 16 control units from the control device 14 discrete signals coming from the rocket (anti-missile, torpedoes, guided missile, launch container, etc.) 32 _i through, respectively, the second and / or seventh groups of outputs , the sixth group of inputs of the motor drive current disconnectors 17; from the fourth groups of outputs of the main 15 and / or backup 16 control units from the control device 14, discrete signals are output to the third groups of inputs, respectively, of the main 20 and / or duplicate 21 switching units from the power supply device 19, in which the switching elements operate, which ensures the transfer of control discrete signals to a change in position (return to the initial position) of the motor drive of current disconnectors 17 from the main 28 and / or backup 29 power supply units the auxiliary drive of current disconnectors from the power supply device 19, arriving at the fourth inputs of the main 20 and / or the backup 21 switching units, through the second groups of outputs of the main 20 and / or the backup 21 switching units from the power supply device 19 to the tenth and / or twelfth groups of motor inputs drive current disconnectors 17; algorithm 1 is executed; Algorithm 3 is executed (Algorithm 7);

j) display of information about the sequence, content and results of initializing the functional software of the firing command and control information system on the first 8 and second 9 monitors from the automated workstation of operator 1;

k) automatic or at the operator’s command (in the “operator-computer complex” dialogue mode using the first 4 and second 5 keyboards) paper-based documentation of the results of initialization of functional command-shooting software

information management system using the first 6 and second 7 documenting devices from the workstation of operator 1;

m) automatic storage in the memory of the first 2 and second 3 computer systems from the automated workstation of operator 1 of the initialization of the functional software of the command-firing information-control system.

Duty stage

The preparatory phase of the command-firing information management system is completed. Periodically, in accordance with the algorithm of the operation of the firing command and control information system, sequentially or in parallel for each peripheral communication subsystem 13 ₁ ÷ 13 _n , the first 2 and second 3 computing complexes from the automated workstation of operator 1 automatically, under the control of a system or functional software command-firing information management system, or manually by the operator, in the dialogue mode "operator - computer complex" using calling the first 4 and second 5 keyboards from the automated workstation of operator 1, is carried out:

a) testing of digital channels of information exchange 12 _1-1 ÷ 12 _1-n , 12 _2-1 ÷ 12 _2-n organization of information exchange:

- through digital channels of information exchange 12 _1-1 ÷ 12 _1-n honey with the first computing complex 2 from the automated workstation of operator 1 and the main 15, duplicating 16 control units and functional check units 18 from the composition of control devices 14 of peripheral communication subsystems 13 ₁ ÷ 13 _n ;

- through digital channels of information exchange 12 _2-1 ÷ 12 _{2-n to the} honey of the second computing complex 3 from the automated workstation of the operator 1 and the main 15, duplicating 16 control units and functional check units 18 of the control devices 14 of the peripheral communication subsystems 13 ₁ ÷ 13 _n ;

b) synchronization of the time generated by the means of the first 2 and second 3 computing complexes with the time generated by the first 10 and second 11 base stations of the single time system with remote antennas from the automated workstation of operator 1, respectively;

c) entering into the memory of the first 2 and second 3 computer complexes from the automated workstation of operator 1 data about the operator of the firing command and control information system (when changing the operator);

d) the reassignment of the first computing complex 2 - the main, and the second computing complex 3 - duplicate, from the workstation of operator 1 or, conversely;

e) control of the position of the motor drives of current disconnectors 17 from the composition of control devices 14 of peripheral communication subsystems 13 ₁ ÷ 13 _{n by} sequential execution of algorithms 1-3;

f) checking the serviceability of the switching elements from the main 20, duplicating 21 switching units, as well as checking the serviceability of the main 22, duplicating 23 blocks of secondary power supplies, the main 24 and duplicating 25 command supply units for the operation of the squibs from the power supply devices 19 of the peripheral communication subsystems 13 ₁ ÷ 13 _n execution of algorithm 4;

g) checking the serviceability (current state) of the mating elements of the command-firing information-control system 33 ₁ ÷ 33 _{n by} performing algorithm 5;

h) checking the sequence and correctness of the operations for preparing and launching missiles (anti-missiles, torpedoes, guided missiles, etc.) 32 ₁ ÷ 32 _{n by} performing algorithm 6;

i) checking the health of motor drives of current disconnectors 17 from the composition of control devices 14 of peripheral communication subsystems 13 ₁ ÷ 13 _{n by} performing algorithm 7;

j) hardware and software testing:

- the first 2 and second 3 computing complexes, the first 4 and second 5 keyboards, the first 6 and second 7 documentation devices, the first 8 and second 9 monitors, the first 10 and second 11 base stations of the single time system with remote antennas from the automated workstation of the operator one;

- the main 15, duplicating 16 control units and a functional check unit 18 of the control devices 14 of the peripheral communication subsystems 13 ₁ ÷ 13 _n ;

k) display of the content and results of the functional software of the firing command and control information system on the first 8 and second 9 monitors from the automated workstation of operator 1;

l) documenting on paper the contents and results of the functional software of the firing command and control information system using the first 6 and second 7 documenting devices from the workstation of operator 1;

m) storing in memory of the first 2 and second 3 computing systems from the automated workstation of operator 1 of the content and results of the functional software of the command-firing information-control system.

Main stage

The preparatory phase of the command-firing information management system is completed. In accordance with the algorithm for the operation of the command-fire information-control system in series or in parallel for each peripheral communication subsystem 13 ₁ ÷ 13 _n , the first 2 and second 3 computing complexes from the automated workstation of the operator 1 automatically, under the control of the functional software of the command-fire information management system, or manually by the operator, in the dialogue mode “operator - computer complex” using the first 4 and second 5 cl Viaturas from the operator’s automated workstation 1 (signal transceiver between the first 2 or second 3 computing complex and the main 15, duplicating 16 control units and functional check units 18 from the control devices 14 through digital channels of information exchange 12 _1-1 ÷ 12 _1- 12 _n or _2-1 ÷ February _12-n is carried out:

a) transfer of motor drives of current disconnectors 17 from the composition of control devices 14 of peripheral communication subsystems 13 ₁ ÷ 13 _n to a position in which the fifth groups of outputs and sixth groups of inputs of the main 15 and duplicate 16 control units from the composition of control devices 14, second groups of outputs and first groups of inputs of the main 20 and duplicating 21 switching units from the composition of power supply devices 19, respectively, are connected through the fifth groups of outputs and sixth groups of inputs of the motor drives of current disconnectors 17 with rockets (anti ballistic missiles, torpedoes, guided missiles, launch containers, etc.) 32 ₁ ÷ 32 _n , for which:

- from the fourth groups of outputs of the main 15 and / or duplicating 16 control units from the composition of the control devices 14, discrete signals are output to the third groups of inputs, respectively, of the main 20 and / or duplicating 21 switching units from the composition of the power supply 19, in which the switching elements operate that ensures the transfer of control discrete signals to change the position of the motor drives of current disconnectors 17 from the main 28 and / or backup 29 power supply units of the motor drives of current disconnectors from the composition of power supply devices 19, arriving at the fourth inputs of the main 20 and / or duplicating 21 switching units, through the second groups of outputs of the main 20 and / or duplicating 21 switching units from the composition of power supply devices 19, respectively, to the tenth and / or twelfth groups of motor inputs current disconnector drives 17;

- checks the execution of the command to change the position of the motor drives of the current disconnectors 17 from the composition of the control devices 14, in which the fifth groups of outputs and sixth groups of inputs of the main 15 and the backup 16 control units from the composition of control devices 14, the second groups of outputs and the first groups of inputs of the main 20 and duplicating 21 switching units from the composition of power supply devices 19, respectively, are connected through fifth groups of outputs and sixth groups of inputs of motor drives of current disconnectors 17 with s (interceptor missiles, torpedoes, guided missiles, launch canisters and the like) 32 ₁ 32 ÷ _n, for which outputs from the fifth main group 15 and / or redundant control 16 from the control device 14 blocks issued digital signals, respectively, the first and / or eighth groups of inputs of the motor drives of current disconnectors 17, followed by reading from the sixth groups of inputs of the main 15 and / or duplicating 16 control units from the control devices 14 discrete signals coming from the second and / or seventh UPP outputs of motor drives current disconnectors 17;

- checks the correct connection of missiles (anti-missiles, torpedoes, guided missiles, launch containers, etc.) 32 ₁ ÷ 32 _n , for which, from the fifth groups of outputs of the main 15 and / or duplicating 16 control units from the composition of control devices 14 discrete signals, respectively, to the first and / or eighth groups of inputs and then from the fifth groups of outputs of the motor drives of current disconnectors 17 to missiles (anti-missiles, torpedoes, guided missiles, launch containers, etc.) 32 _i , followed by reading from the sixth groups inputs main 15 and / or duplicating 16 control units from the control devices 14 discrete signals coming from missiles (missiles, torpedoes, guided missiles, launch containers, etc.) 32 ₁ ÷ 32 _n through, respectively, the second and / or seventh groups outputs, sixth groups of inputs of motor drives of current disconnectors 17;

b) synchronization of the time generated by the means of the first 2 and second 3 computing complexes with the time formed, respectively, by the first 10 and second 11 base stations of the single time system with remote antennas from the automated workstation of operator 1;

c) monitoring the current state of the mating elements of the command-firing information-control system 33 ₁ ÷ 33 _{n by} issuing from the second groups of outputs and reading from the third groups of inputs of the main 15 and / or duplicating 16 control units from the control devices 14 of the peripheral communication subsystem 13 ₁ ÷ 13 _n discrete and analog signals;

d) input of initial data into the on-board equipment of missiles (anti-missiles, torpedoes, guided missiles, etc.) 32 ₁ ÷ 32 _n , for which purpose from the fifth groups of outputs of the main 15 and / or duplicating 16 control units from the composition of control devices 14 through the first and / or eighth input groups and fifth output groups of motor drives of current disconnectors 17 transmit signals to missiles (anti-missiles, torpedoes, guided missiles, etc.) 32 ₁ ÷ 32 _n ;

e) checking the correctness of input of the initial data into the on-board equipment of missiles (anti-missiles, torpedoes, guided missiles, etc.) 32 ₁ ÷ 32 _{n by} reading discrete signals arriving at the sixth groups of inputs of the main 15 and / or duplicating 16 control units from the device control 14 from missiles (anti-missiles, torpedoes, guided missiles, launch containers, etc.) 32 ₁ ÷ 32 _n through, respectively, the second and / or seventh groups of outputs, sixth groups of inputs of motor drives of current disconnectors 17;

f) the preparation and launch of missiles (missile defense, torpedoes, guided missiles, etc.) 32 ₁ ÷ 32 _n , for which, in accordance with the training and launch sequence diagram, implemented as part of the functional software for command and fire information control system: from the fourth groups of outputs of the main 15 and / or duplicating 16 control units from the composition of the control devices 14, discrete signals are issued / removed to / from the third (s) groups / groups of inputs, respectively, of the main 20 and / or duplicate 21 blocks

switching from the composition of power supply devices 19, in which switching elements are turned on / off, which ensures the appearance / disappearance of discrete and / or analog signals on board missiles (missiles, torpedoes, guided missiles, etc.) 32 ₁ ÷ 32 _n from the main 22 and / or duplicating 23 blocks of secondary power supplies, and / or from the main 24 and / or duplicating 25 blocks of command for triggering the igniter through the sixth and seventh groups of inputs, the second group of outputs of the main 20 and / or duplicating 21 switching blocks and from the composition of power supply devices 19, respectively, tenth and twelfth groups of inputs, fifth groups of outputs of motor drives of current disconnectors 17 from the composition of control devices 14; from the fifth groups of outputs of the main 15 and / or duplicating 16 control units from the control devices 14, discrete and / or analog signals arriving at the missiles (anti-missiles, torpedoes, guided missiles, etc.) are given / removed in the necessary sequence 32 ₁ ÷ 32 _n through the first and / or eighth groups of inputs, fifth groups of outputs of the motor drives of current disconnectors 17 from the composition of control devices 14; missiles (anti-missiles, torpedoes, guided missiles, etc.) 32 ₁ ÷ 32 _n , depending on the signals coming from the fifth groups of inputs of the motor drives of current disconnectors 17, and their technical condition, form discrete and / or analog signals arriving at sixth groups of inputs of the main 15 and / or duplicating 16 control units from the control devices 14 through the sixth groups of inputs, respectively, the second and seventh groups of outputs of the motor drives of current disconnectors 17; discrete and analog signals are fed to the sixth groups of inputs of the main 15 and / or duplicating 16 control units from the control devices 14;

g) display of the content and results of the functional software of the firing command and control information system on the first 8 and second 9 monitors from the automated workstation of operator 1;

h) documenting on paper the contents and results of the functional software of the firing command and control information system using the first 6 and second 7 documenting devices from the workstation of operator 1;

i) storing in memory of the first 2 and second 3 computer systems from the automated workstation of operator 1 of the content and results of the functional software of the command-firing information-control system.

Emergency phase

At the preparatory, on-duty and main stages when functional software detects a command-fire information-control system and / or an operator signs of abnormal operation of a command-fire information-control system and / or missile (anti-missiles, torpedoes, guided missiles, etc.) 32 ₁ ÷ 32 _n , which adversely affect the safety of operation and / or the intended use of the firing command and control information system or missiles (missiles, torpedoes, guided missiles and etc.) 32 ₁ ÷ 32 _n , carried out:

a) termination of current operations and localization of signs of abnormal operation of the command-firing information-control system and / or missiles (missiles, torpedoes, guided missiles, etc.) 32 ₁ ÷ 32 _n , while:

- if signs of an abnormal situation are detected at the standby stage and their localization is ensured by the reassignment of computer systems, then the operator manually, in the operator-computer complex dialogue mode, uses the first 4 and second 5 keyboards from the workstation of operator 1 to reassign the computer systems ( a duplicate computing complex is designated as the main one, and the main computing complex as the duplicate one);

- if signs of an abnormal situation are found during the preparation and launch of missiles (missiles, torpedoes, guided missiles, etc.) 32 ₁ ÷ 32 _n , in accordance with the cyclogram for the execution of jack-off operations, implemented as part of the functional software of the command firing information-control system, from the fourth groups of outputs of the main 15 and / or duplicating 16 control units from the composition of the control devices 14 in the necessary sequence are issued / removed discrete signals to / from the third (s) g ruppa / groups of inputs, respectively, of the main 20 and / or duplicating 21 switching units from the power supply devices 19, in which switching elements are turned on / off, which ensures the discharge of missile power sources (anti-missiles, torpedoes, guided missiles, etc.) 32 ₁ 32 ÷ _n through sixth input group, ninth and / or eleventh group tokorazediniteley motor drive output 17 from the control device 14, the first group of inputs and outputs of the fifth main group 20 and / or 21 overlapping the switching units on axes ovnye 26 and redundant blocks 27 from the discharge power supply device 19;

b) displaying the content and results of the functional software of the command-firing information-control system on the first 8 and second 9 monitors from the automated workstation of operator 1 (if they are in good condition);

c) documenting on paper the contents and results of the functional software of the firing command and control information system using the first 6 and second 7 documenting devices from the workstation of operator 1 (if they are in good condition);

d) storing in memory of the first 2 and second 3 computer systems from the automated workstation of operator 1 of the content and results of the functional software of the command-firing information-control system (if they are in good condition).

Maintenance Phase

Actions are carried out in a different sequence, corresponding to the preparatory, duty and main stages of the command-firing information-control system in which it is allowed:

- to each of the motor drives of current disconnectors 17 control devices 14 from the composition of the peripheral communication subsystems 13 ₁ ÷ 13 _n through the sixth group of inputs and the fifth group of outputs instead of a rocket (anti-missile, torpedoes, guided missile, launch container, etc.) 32 _i its functional simulator;

- connect the functional simulators instead of peripheral communication subsystems 13 ₁ ÷ 13 _n to the first computing complex 2 from the automated workstation of operator 1 using digital information exchange channels 12 _1-1 ÷ 12 _1-n , and to the second computing complex 3 from the composition automated workstation of operator 1 using digital channels of information exchange 12 _2-1 ÷ 12 _2-n instead of peripheral communication subsystems 13 ₁ ÷ 13 _n to connect their functional simulators;

- to each of the main 15 and duplicating 16 control units of control devices 14 from the composition of the peripheral communication subsystems 13 ₁ ÷ 13 _n, through the second groups of outputs and third groups of inputs, connect instead of the mating elements of the firing command and control information system (for example, doors, hatches, protective devices, microclimate maintenance devices, etc.) 33 _i their functional imitators;

- to each first group of inputs and outputs of the main 15 and duplicating 16 control units, as well as function test units 18 of the control devices 14 of the peripheral communication subsystems 13 ₁ ÷ 13 _n, connect instead of the first computing complex 2 and the second computing complex 3 of the automated working operator’s places 1 their functional simulators.

At all stages of work, the interaction of a device or operator with supporting systems can be carried out through specialized and unified digital, radio-relay, television, telegraph, telephone, sound, voice, etc. channels of information exchange with supporting systems. In this case, the input of data from the supporting systems into the first computing complex 2 and the second computing complex 3 from the automated workstation of operator 1 is carried out through specialized converters corresponding to the type of information exchange channel with the supporting systems, and / or by the operator manually in the dialog “operator - computing” complex ”using the first 4 and second 5 keyboards.

Exact time synchronization of missile preparation and launch operations (anti-missiles, torpedoes, guided missiles, etc.) 32 ₁ ÷ 32 _n with the operation of supporting systems, as well as precise fulfillment of the time schedule for prelaunch and launch - missile preparation and launch cyclograms (anti-missile , torpedoes, guided missiles and the like) 32 ₁ 32 _n ÷ carried out by means of time synchronization generated by means of the first 2 and second 3 computer systems, with the time, formed by respectively the first 10 and second 11 mill base they use a single time system with remote antennas from the automated workstation of operator 1. The first 10 and second 11 base stations of a single time system with remote antennas from the automated workplace of operator 1 create and store long-term time scales synchronized with the scale of the State common time service and reference frequencies, with which, in turn, the operating time scale of the supporting systems is synchronized.

This device compared to the prototype with respect to missiles (missiles, torpedoes, guided missiles, etc.) allows you to:

- to carry out accurate time synchronization of the preparation and start-up operations with the work of the supporting systems, to accurately perform the time

regulations for prelaunch and launch, which expands the functionality of the device;

- protect against unauthorized control actions and carry out jacking operations in the event of a failed start, which increases the safety of the device;

- conduct autonomous and comprehensive checks of the functioning of the command-firing information management system, including with simulated execution of preparation and start-up operations, which increases the reliability and fault tolerance of the device.

The use of the invention in armaments and military equipment allows us to successfully carry out combat missions (for example, hitting targets or delivering warheads to a certain point in space), which directly depend on the time (maternity, astronomical, relative, etc.) of the preparation and launch operations one and / or a group of missiles (anti-missiles, torpedoes, guided missiles, etc.).

Claims (1)

Command-firing information management system containing an automated workstation of the operator, equipped with two computer systems, two keyboards, two documentation devices and two monitors, peripheral communication subsystems according to the number of missiles being prepared for launch, anti-missiles, torpedoes, guided missiles, digital information exchange channels in an amount corresponding to the number of peripheral communication subsystems or a multiple exceeding the number of peripheral communication subsystems, which consists of two additional base stations of a single time system with external antennas introduced into the operator’s automated workstation, a control device consisting of a main and backup control units, a motor drive of current disconnectors and a functional check unit in each peripheral communication subsystem power supply, consisting of the main and backup blocks of switching, the main and backup blocks of secondary power supplies, the main and backup blocks under There are commands for triggering the squibs, the main and backup blocks of the discharge, the main and backup power supplies of the motor drive of the current disconnectors, the main and backup blocks of the standby power supply, and a keyboard and a device are connected to each computer complex from the operator’s automated workstation using digital data exchange channels documentation, monitor, base station of a single time system with remote antennas, through the first groups of inputs main / d duplicating control units and function testing units from the control devices of the peripheral communication subsystems, each power supply device from the peripheral communication subsystems through the inputs of the main and backup blocks of secondary power supplies, the main and backup power supply units for triggering the squibs, the main and backup power supplies of the motor drive current disconnectors, main and backup standby power supply units connected to an external power source I, the outputs of the main and backup power supply standby units are connected to consumers from the power supply and control devices, the outputs of the main and backup power supply units of the motor drive of current disconnectors, the main and backup power supply units for ignition actuators, the main and backup power supply units of the secondary power supply are connected respectively to the fourth inputs, the sixth and seventh groups of inputs of the main and backup switching units, the fifth output groups of which are connected to odes of the main and backup blocks of the discharge, the second groups of outputs to the tenth and twelfth groups of inputs of the motor drive of current isolators, the third groups of inputs of the main and backup blocks of switching are connected to the fourth groups of outputs of the main and backup control units, and the first groups of inputs to the ninth and eleventh groups outputs of the motor drive of current disconnectors, each of the main and backup control units of control devices from the composition of the peripheral communication subsystems of the second groups in outputs and the third groups of inputs connected to the mating elements of the command-firing information-control system, the fifth groups of outputs to the first and eighth groups of inputs of the motor drive of current disconnectors, the sixth groups of inputs to the second and seventh groups of outputs of the motor drive of current disconnectors, each of the motor drives of current disconnectors control devices from the composition of the peripheral communication subsystems of the sixth group of inputs and the fifth group of outputs connected to a rocket, anti-missile, torpedo, control The projectile being launched, the launch container, and the third group of inputs and the fourth group of outputs are connected respectively to the second group of outputs and the third group of inputs of the function test block.